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Patent Searching and Data


Title:
CONTROL MOMENT GYROSCOPE
Document Type and Number:
WIPO Patent Application WO/2014/157798
Kind Code:
A1
Abstract:
The objective of the present invention is to provide a control moment gyroscope which can be provided in a limited space since the volume thereof can be reduced without a change in performance by optimizing the shapes and mounting positions of each component. To this end, the control moment gyroscope of the present invention is a control moment gyroscope for generating torque in the orthogonal directions to both of two shafts which are perpendicularly disposed to each other by rotating the two shafts, and the control moment gyroscope comprises: a gimbal motor formed in the shape of a hollow cylinder and supplying momentum; spin motor provided to the inside of the gimbal motor and supplying momentum in a perpendicular direction to the momentum of the gimbal motor; and a flywheel provided to the inside of the gimbal motor and supplied with the rotational force of the gimbal motor and the rotational force of the spin motor.

Inventors:
LEE SEON HO (KR)
Application Number:
PCT/KR2013/009575
Publication Date:
October 02, 2014
Filing Date:
October 25, 2013
Export Citation:
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Assignee:
KOREA AEROSPACE RES INST (KR)
International Classes:
B64G1/28; G01C19/30; G05D1/08
Foreign References:
US20100000349A12010-01-07
KR20090116690A2009-11-11
US5386738A1995-02-07
US5425281A1995-06-20
US6834561B22004-12-28
Other References:
See also references of EP 2955114A4
Attorney, Agent or Firm:
MI PATENT & LAW FIRM (KR)
특허법인 명인 (KR)
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